Memory Items And Standard Calls

Question 1

Cabin Altitude

Answer 1

1. Don the oxygen masks
2. Establish crew communuications
3. Check the cabin altitude and rate (PM)
4. If the cabin Altitude is uncontrollable:

Pax Oxy on……………………..Push to ON hold for 1 sec (PM)

Without delay descend to the lowest safe altitude or 10,000 feet whichever higher. If fuel is critical descend to 14,000 feet. PF call “rapid descent”

Thrust Levers Idle
Extend Speedbrakes
If structural integrity in doubt limit speed
Descended at VMO/MMO

PM confirm all actions done during descent

Note/ if maintaining 14,000ft PA “all occupants remain on O2”. 10,000ft PA “pax may come off O2”.

5. The cab altitude is controllable, continue normal operation

Question 2

Aborted engine start L, R

Answer 2

Fuel control switch (affected site)………Cut off

This is the memory item for aborting engine start without EICAS message. On completion of memory item do NNC

Question 3

Dual engine fail/stall

Answer 3

1. Fuel control switches (both)……………. CUT
   OFF THEN RUN
2. Ram air turbine switch………………….. push
   and hold for one second

Note. Setting 2000 on MCP provides info on where you will be at circuit altitude. Captain fly HDG SEL FLCH start heading direct alternate.
After restarting 1 engine get multiple EICAS message, some relevant, some not. 1 centre tank pump latched off (can’t be resolved)

Question 4

Engine auto start L, R

Answer 4

Fuel control switch (affected side)……… confirm……….. cut off

(Confirmation only required in the air)

During ground starts, parameters that the Autostart monitors and attempt to correct are:

• Compressor Stall
• Hot Start
• Hung Start
• No EGT rise
• Loss of one Starter
• Start Time exceeds the starter duty cycle timer

The Autostart aborts for:

• Loss of both starters
• No N1 rotation

Question 5

Engine limit exceeded L, R

Answer 5

1. (affected side) A/T arm switch………. Confirm……. Off
2. Thrust lever (affected side)…… confirm…. retard until limit exceed message blanks
   or the thrust lever is at idle 

Question 6

Engine surge L, R

Answer 6

1. A/T arm switch (affected side)…… …….confirm…………….. off
2. Thrust lever (affected side)…… Confirm…… retard until the engine surge message blanks or the thrust lever is at idle

Question 7

Engine severe damage/separation L, R

(Note severe damage requires indication plus vibration)

Answer 7

1. A/T arm switch (affected side)…………. CONFIRM……… OFF (PF)
2. Thrust lever (affected side)………… confirm…………… Idle (PF)
3. Fuel control switch (affected side)…….. confirm………. Cut off
4. Engine fire switch (affected side)………… confirm……….pull

Question 8

Fire engine L,R (IN FLIGHT)

Note. Ground fire not memory item

Answer 8

1. A/T arm switch (affected side)……….. confirm…………. Off
2. Thrust lever (affected side)………………confirm………….Idle
3. Fuel control switch (affected side)……confirm………….Cutoff
4. Engine fire switch (affected side)……..confirm………….Pull

If the fire engine message stays showing:

5. Engine fire switch (affected side) ……rotate to the stop and hold for one second

Question 9

[ ] Stabilizer

Answer 9

1. Stab cut out switches (both)………………… cutout
2. Do not exceed the current airspeed

Question 10

Airspeed unreliable

Answer 10

1. Auto pilot disconnect switch………………..push
2. A/T arm switch (both)…………………… …….off
3. F/D switches (both)………………….. ………..off
4. Set the following gear up pitch attitude and thrust:Flaps extended………………….. 10° and 85% N1
   Flaps up………………………………. 4° and 70% N1

Question 11

Deviation Calls on Approach

Calls made after FAF/FAP, if deviation below 1000ft follow call with “unstable”

Answer 11

Lateral path:

ILS/GLS/VOR or LOC >1 dot “TRACK”

RNAV Flashing deviation pointer “TRACK”
or amber scale.

Vertical path:

ILS/GLS >1 dot “GLIDEPATH”

RNAV Flashing deviation pointer “GLIDEPATH”
or amber scale.